Wind tunnel testing of composite wing flutter speed due to control surface excitation
Flutter is a dynamic instability problem represents the interaction among aerodynamic forces and structural stiffness during flight. The study was conducted to investigate whether deflecting the control surface will affect the flutter speed and the flutter frequency. A wind tunnel test was performed...
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| Main Author: | |
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| Format: | Conference or Workshop Item |
| Published: |
2012
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| Subjects: | |
| Online Access: | http://eprints.utm.my/id/eprint/47821/ http://dx.doi.org/10.4028/www.scientific.net/AMM.315.359 |
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| Institution: | Universiti Teknologi Malaysia |